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Volumn , Issue , 2005, Pages 12749-12762

The M-DAW project investigations in novel wing tip device design

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT EFFICIENCY; ART TECHNOLOGY; CRYOGENIC TEMPERATURES; WING TIP DEVICE;

EID: 30744469605     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (12)

References (14)
  • 4
    • 84888776176 scopus 로고
    • Boeing, Seattle, US Patent for "High Taper Wing Tip Extension", No. 5,039,032, filed 19 May
    • Rudolph P. K. C., Boeing, Seattle, US Patent for "High Taper Wing Tip Extension", No. 5,039,032, filed 19 May 1989
    • (1989)
    • Rudolph, P.K.C.1
  • 5
    • 84888804401 scopus 로고    scopus 로고
    • Boeing, Seattle, US Patent for "Blunt Leading Edge Raked Wingtips", No. 6,089,502, filed 12 Jun
    • Herrick L. L. et al, Boeing, Seattle, US Patent for "Blunt Leading Edge Raked Wingtips", No. 6,089,502, filed 12 Jun 1998
    • (1998)
    • Herrick, L.L.1
  • 6
    • 84888807382 scopus 로고
    • US Patent for "Twisted Wing Tip Fin", No. 2,576,981, filed
    • Vogt R., US Patent for "Twisted Wing Tip Fin", No. 2,576,981, filed 1951
    • (1951)
    • Vogt, R.1
  • 7
    • 2942727310 scopus 로고
    • A design approach and selected wind-tunnel results at high subsonic speeds for wing-tip mounted winglets
    • Whitcomb R. T., A Design Approach And Selected Wind-Tunnel Results At High Subsonic Speeds For Wing-Tip Mounted Winglets, NASA TN D-8260, 1976
    • (1976) NASA TN , vol.D-8260
    • Whitcomb, R.T.1
  • 8
    • 84888792050 scopus 로고    scopus 로고
    • Wessling, Germany, US Patent for "Wing Tip Extension for a Wing", No. 6,722,615, filed 5 Apr
    • Heller G., Fairchild Dornier, Wessling, Germany, US Patent for "Wing Tip Extension for a Wing", No. 6,722,615, filed 5 Apr 2002
    • (2002)
    • Heller, G.1    Dornier, F.2
  • 9
    • 84888781760 scopus 로고
    • British Aerospace, London, US Patent for "Aircraft Wing and Winglet Arrangement", No. 4,714,215, filed 12 Jun
    • Jupp J. A., Rees P. H., British Aerospace, London, US Patent for "Aircraft Wing and Winglet Arrangement", No. 4,714,215, filed 12 Jun 1986
    • (1986)
    • Jupp, J.A.1    Rees, P.H.2
  • 10
    • 84888782692 scopus 로고
    • Seattle, US Patent for "Spiroid Tipped Wing", No. 5,102068, filed 25 Feb
    • Gratzer, L. B., Seattle, US Patent for "Spiroid Tipped Wing", No. 5,102068, filed 25 Feb 1991
    • (1991)
    • Gratzer, L.B.1
  • 11
    • 84888793941 scopus 로고    scopus 로고
    • France, European Patent for "Cylindrical Wing Tip with Helical Slot", No. WO 02/083497, filed 11 Apr
    • Hugues, C., Vitry sur Seine, France, European Patent for "Cylindrical Wing Tip with Helical Slot", No. WO 02/083497, filed 11 Apr 2001
    • (2001)
    • Hugues, C.1    Seine, V.S.2
  • 14
    • 84888801950 scopus 로고    scopus 로고
    • Two-point-design of nonplanar lifting configurations using a databased aerodynamic prediction tool
    • Büscher A., Streit T., Two-Point-Design of Nonplanar Lifting Configurations Using a Databased Aerodynamic Prediction Tool, DGLR Jahrbuch, Vol. I, pp. 319-327, 2004
    • (2004) DGLR Jahrbuch , vol.1 , pp. 319-327
    • Büscher, A.1    Streit, T.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.